# Service difficulty reports: N607LR

A list on [N607LR](https://openairdocs.org/aircraft/N607LR.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 224 reports

- [SDR REXA2024071200518](https://openairdocs.org/sdr/REXA2024071200518.md): Control Lever · inoperative · Jul 6, 2024 · N607LR · Cndair CL6002D24 · Landing Gear Selector
  > ON FINAL APPROACH GEAR DISAGREE WARNING MESSAGE DISPLAYED. FOLLOWED QRH PROCEDURE AND USED GEAR MANUAL RELEASE AND RECEIVED THREE GREEN INDICATIONS FOR THE LANDING GEAR. REMOVED AND REPLACED LANDING GEAR LEVER IAW CRJ 900 AMM 32-31-01. PERFORMED OPS CHECK AN
- [SDR REXA2024103101308](https://openairdocs.org/sdr/REXA2024103101308.md): Seat Track · corroded · Apr 3, 2024 · N607LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > UPON INSTALL, FOUND SEAT TRACK TO BE CORRODED AND FOUND TO BE OUT OF LIMITS, REQUIRES REPLACEMENT. REPLACED LBL9.00 AND RBL 9.00 SEAT TRACK SEGMENTS BETWEEN F.S 693.00-F.S.847.00 I.A.W. MHIRJ REO 670-53-00-598 REV.C, DATED 2023-02-08.
- [SDR REXA2024110101405](https://openairdocs.org/sdr/REXA2024110101405.md): Nut Plate · corroded · Jan 3, 2024 · N607LR · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > DOUBLER AT STGR 27 BETWEEN FS 409.00 AND 421.00. (FOUND TO BE CORRODED) CORROSION HAS DEEP PITTING AROUND PLUG CUTOUT FOR ANTENNA CHANNEL DOUBLER AND IS BEYOND REPAIRABLE LIMITS PROVIDED IN CRJ900 SRM 53-21-01-101-006-A04. ADDITIONALLY, NO DAMAGE ALLOWED IN
- [SDR REXA2024110101404](https://openairdocs.org/sdr/REXA2024110101404.md): Doubler · corroded · Dec 23, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DOUBLER AT STRINGER 27 BETWEEN FS 295.00 AND 310.00 IS CORRODED. REMOVED, LOCATED AND DRILLED NEW SERVICEABLE TCAS DOUBLER P/N: SH670-32364-7S IAW CRJ 900 51-40-11-001-001-A01, AND INSTALLED IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2024110101403](https://openairdocs.org/sdr/REXA2024110101403.md): Support Beam · chafed · Dec 23, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD AND AFT ENDS OF SUPPORT BEAM ARE CHAFED. CHAFES ARE APPROX 0.125 WIDE, 0.125 WIDE, AND 0.050 DEEP. REPAIRED AFT CARGO DOOR SUPPORT BEAM IAW ENDEAVOR AIR EA CRJ953-15861
- [SDR REXA2024103101335](https://openairdocs.org/sdr/REXA2024103101335.md): Buttstrap · corroded · Dec 20, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S. 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 26L AND STGR 26R. REPAIRED IAW ENDEAVOR AIR EA CRJ953-15722 REV A
- [SDR REXA2024103101334](https://openairdocs.org/sdr/REXA2024103101334.md): Frame · corroded · Dec 16, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Frame
  > WHERE STRINGER 22R MEETS FRAME AT FS349.00 THERE IS CORROSION ON FRAME INSTALLED NEW FRAME AT FS 349 BETWEEN STR 24R TO STR 18R IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 P/N SH670-32035-1
- [SDR REXA2024110601428](https://openairdocs.org/sdr/REXA2024110601428.md): Stringer · corroded · Dec 10, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R IS CORRODED BETWEEN FS 333.00 AND 349.00. REMOVED AND REPLACED CLIP PN SH670-35625-2 AT STGR 22R BETWEEN FS 333-349 IAW CRJ 900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024103101333](https://openairdocs.org/sdr/REXA2024103101333.md): Stringer · corroded · Dec 10, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AFTER REMOVAL OF INTERCOSTAL FOUND CORROSION AT STR20R BETWEEN FS 319 TO FS 349. REMOVED STR20R BETWEEN FS 319 TO FS 349 IAW CRJ-900 SRM 51-42-06-001-001-A01 CORRECTIVE ACTION: INSTALLED STR20R BETWEEN FS 319 TO FS 349 IAW CRJ 900 SRM 51-42-06/21-001-001
- [SDR REXA2024103101332](https://openairdocs.org/sdr/REXA2024103101332.md): Intercostal · deformed · Dec 10, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND ELONGATED HOLES AT THE INTERCOSTAL AND 2 CLEATS AT LEVEL OF FS 333.00 AND STR 20R. REMOVED DAMAGED INTERCOSTAL AND CLEATS (2 E/A) LOCATED BETWEEN FS 319 TO FS 349 AND STR 20R IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED N
- [SDR REXA2024022600214](https://openairdocs.org/sdr/REXA2024022600214.md): Web · corroded · Dec 5, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR FWD STAIR WEB CORRODED. REMOVED FWD STAIR WEB STIFFENING ANGLES, LOCATED AND DRILLED NEW SERVICEABLE FWD STAIR WEB PN 601R317071-12 AND INSTALLED STIFFENING ANGLES ONTO NEW WEB IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REFERE
- [SDR REXA2024110101402](https://openairdocs.org/sdr/REXA2024110101402.md): Stringer · corroded · Dec 3, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R IS CORRODED BETWEEN FS 394.00 TO 409.00, FS 421.00 TO 437.00, AND FS 469.00 TO 485.00. REMOVED AND REPLACED STRINGER 21R (PN SH670-31385-1) IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2024103101305](https://openairdocs.org/sdr/REXA2024103101305.md): Floorbeam · corroded · Dec 2, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH FS280 CROSS BEAM HAS MINOR CORROSION INSTALLED NEW SERVICEABLE L/H FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-13-001-001-A01 AND REFERENCED SB 670BA-53-041 REV M FOR FASTENER CALL OUT
- [SDR REXA2024110101401](https://openairdocs.org/sdr/REXA2024110101401.md): Web · corroded · Dec 1, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR AFT STAIR WEB CORRODED. REMOVED AFT STAIR WEB STIFFENING ANGLES, LOCATED AND DRILLED NEW SERVICEABLE AFT STAIR WEB PN 601R317071-11 AND INSTALLED STIFFENING ANGLES ONTO NEW WEB IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REFERE
- [SDR REXA2024103101331](https://openairdocs.org/sdr/REXA2024103101331.md): Stringer · corroded · Dec 1, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AT STRINGER 19R BETWEEN FS 319 TO FS 349 REMOVED AND REPLACED STRINGER 19R, PN SH670-32427-1, BETWEEN FS 319-349 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01
- [SDR REXA2024103101330](https://openairdocs.org/sdr/REXA2024103101330.md): Stringer · corroded · Dec 1, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 20R IS CORRODED BETWEEN FS 581 AND FS 597 REPAIRED IAW ENDEAVOR AIR EA NO CRJ953-15749
- [SDR REXA2024110101400](https://openairdocs.org/sdr/REXA2024110101400.md): Stringer · corroded · Nov 30, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 19 IS CORRODED BETWEEN FS 437.00 TO 453.00 AND FS 469.00 TO 486.00 REMOVED AND INSTALLED NEW STGR 19R BETWEEN F.S 349 - F.S. 477 IAW CRJ 900 SRM 51-42-06-001-001-A01 (UPON FURTHER INVESTIGATION, CORROSION ON STGR 19R AT F.S. 469 - F.S. 486 IS ACT
- [SDR REXA2024110101398](https://openairdocs.org/sdr/REXA2024110101398.md): Stringer · corroded · Nov 30, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 20R IS CORRODED BETWEEN FS 364.00 TO 333.00 AND FS 394.00 TO 394.00. REMOVED,LOCATED AND DRILLED NEW STGR 20R (P/N SH670-31405-2) AT F.S. 333 TO F.S. 477 IAW CRJ900 SRM 51-40-11-001-001-A01 AND INSTALLED IAW CRJ900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024103101329](https://openairdocs.org/sdr/REXA2024103101329.md): Stringer Splice · corroded · Nov 30, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R SPLICE AT F.S. 477 CIRC. JOINT IS CORRODED. REMOVED AND INSTALLED NEW FS 477 STGR 21R SPLICE P/N SH670-33252-1,IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2024110101397](https://openairdocs.org/sdr/REXA2024110101397.md): Angle · corroded · Nov 29, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR CLIP AT DD7A FWD SIDE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE CLIP AT DD7A FWD P/N:601R318058-1 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2024110101396](https://openairdocs.org/sdr/REXA2024110101396.md): Angle · corroded · Nov 29, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR ANGLE Ï¿½CÏ¿½ AT DD7A MID CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR ANGLE Ï¿½CÏ¿½ AT DD7A P/N:601R317052 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2024110101395](https://openairdocs.org/sdr/REXA2024110101395.md): Intercostal · corroded · Nov 29, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR DD4 AFT CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR DD4 AFT INTERCOSTAL P/N:601R31902-317A IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2024110101394](https://openairdocs.org/sdr/REXA2024110101394.md): Cleat · corroded · Nov 29, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR CLEAT ON FRAME AT FS 313.56 AND DD4 CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR CLEAT P/N:600-31902-269 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2024110101393](https://openairdocs.org/sdr/REXA2024110101393.md): Intercostal · corroded · Nov 29, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD5 FWD SIDE FOUND CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR FWD INTERCOSTAL DD5 P/N:601R318091-5 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2024103101304](https://openairdocs.org/sdr/REXA2024103101304.md): Floorbeam · cracked · Nov 29, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AT F.S.1000, RBL27-36 CROSS BEAM IS CORRDED AT NUT PLATE. REPAIRED CROSS BEAM AT F.S.1000 IAW ENDEAVOR AIR EA NO: CRJ953-15733
- [SDR REXA2024103101303](https://openairdocs.org/sdr/REXA2024103101303.md): Floor Support · corroded · Nov 29, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H FLOOR SILL F.S.985-1000 CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL AT FS 985 TO FS 1000 LH SIDE FLOOR LEVEL IAW EA NO: CRJ953-15782 REV IR DATED:11/18/2023.
- [SDR REXA2024103101302](https://openairdocs.org/sdr/REXA2024103101302.md): Seat Track · corroded · Nov 28, 2023 · N607LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL BETWEEN FS 572 AND FS 661+16 AT STGR 15R IS CORRODED. INSTALLED NEW SIDE SEAT RAIL AT FS 572 AND FS 661+16 AT STGR 15R IAW CRJ900 AMM 53-00-49-400-801(CONFIG A07).
- [SDR REXA2024103101301](https://openairdocs.org/sdr/REXA2024103101301.md): Gusset · deformed · Nov 22, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "GUSSETS ON L/H AND R/H SIDES COMMON TO FWD ""J"" ANGLE AND COCKPIT FLOORBOARD HAS ELONGATED HOLES. REMOVED, LOCATED AND DRILLED, INSTALLED NEW GUSSETS P/N CC670-33467-1, CC670-33467-2 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06/21-001-001-A01. RESTORED SU
- [SDR REXA2024103101300](https://openairdocs.org/sdr/REXA2024103101300.md): Angle · cracked · Nov 22, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 ANGLE AT LBL 12 IS CRACKED INSTALLED NEW SERVICEABLE ANGLE P/N CC670-34099-1SB COMMON TO LBL 12 INTERCOSTAL AND FS 280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2024103101328](https://openairdocs.org/sdr/REXA2024103101328.md): Stringer · corroded · Nov 20, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R IS CORRODED BETWEEN FS 280 AND FS 333. REMOVED CORRODED STRINGER 24R P/N:SH670-31212-2, IAW CRJ900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICABLE STRINGER 24R P/N:SH670-31212-2U, IAW CRJ900 SRM 51-42-06-001-001
- [SDR REXA2023112000988](https://openairdocs.org/sdr/REXA2023112000988.md): Stringer Splice · corroded · Nov 19, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R SPLICE AT F.S. 333 IS HEAVILY CORRODED. REMOVED CORRODED STRINGER SPLICE AND INSTALLED A NEW STRINGER SPLICE #24 (P/N: SH670-32429-4) IAW CRJ900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01.
- [SDR REXA2024110101390](https://openairdocs.org/sdr/REXA2024110101390.md): Stringer · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R IS CORRODED BETWEEN FS 364.00 AND 379.00. REMOVED STGR 23R FROM FS 333-379 AND INSTALLED NEW STGR 23R PN: SH670-31380-1 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2024110101388](https://openairdocs.org/sdr/REXA2024110101388.md): Stringer · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R LONGERON IS CORRODED BETWEEN FS 349 AND FS 364 REMOVED AND REPLACED STRINGER 25R LONGERON BETWEEN F.S.333 TO F.S.364.
- [SDR REXA2024103101327](https://openairdocs.org/sdr/REXA2024103101327.md): Stringer · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R IS CORRDED BETWEEN FS 280 AND FS333 REMOVED AND REPLACED STRINGER 23R FROM FS 280-333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2024103101297](https://openairdocs.org/sdr/REXA2024103101297.md): Bracket · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD CARGO CENTER DOOR SURROUND STRUCTURE FWD H BRACKET AT F.S. 629 IS CORRODED. REMOVED AND REPLACED FORWARD CARGO CENTER DOOR SURROUND STRUCTURE FWD H BRACKET AT F.S. 629 IAW SRM 51-42-22-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024103101296](https://openairdocs.org/sdr/REXA2024103101296.md): Web · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H FS280 LOWER WEB IS CORRODED AT LBL 12 REMOVED CORROSION AT LBL 12 ON FS 280 LOWER WEB IAW CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS OF WEB WAS.040, REMOVED.015 OF MATERIAL AND REMAINING THICKNESS IS.025, WHICH IS OUT OF LIMITS IAW CRJ 900 SR
- [SDR REXA2024103101295](https://openairdocs.org/sdr/REXA2024103101295.md): Web · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H FS 280 LOWER WEB IS CORRODED AT RBL 12 REMOVED CORROSION AT RBL 12 ON FS 280 LOWER WEB IAW SRM 51-21-06-001-001-A01. ORIGINAL THICKNESS OF LOWER WEB IS.040, REMOVED.024 OF MATERIAL AND REMAINING THICKNESS IS.016, WHICH IS OUT OF LIMITS IAW CRJ 900 SRM
- [SDR REXA2024103101294](https://openairdocs.org/sdr/REXA2024103101294.md): Frame · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 549 FRAME SECTOR IS CORRODED AT STGR 17L-18L REPAIRED FRAME SECTOR IAW CRJ900 SRM 53-00-06-201-001-A03
- [SDR REXA2024103101293](https://openairdocs.org/sdr/REXA2024103101293.md): Frame · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT F.S. 533 STGR 17L TO STGR 18L IS CORRODED ON THE FWD AND AFT SIDE. REPAIRED FRAME AT F.S.533 IAW CRJ-900 SRM 53-00-06-201-001-A03
- [SDR REXA2024011600080](https://openairdocs.org/sdr/REXA2024011600080.md): Floorbeam · cracked · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH FS280 CROSSBEAM CORROSION CAP ANGLE IS CRACKED. REMOVED CORRODED WEB AT LBL 12 AND INSTALLED A FABRICATED FS 280 LOWER WEB AND BUTT STRAP. COMPLIED WITH STEPS 5B (1-2) OF CRJ 900 SRM 53-11-10-201-004-A01 FOR REPAIR OF L/H FS 280 LOWER WEB. REFERENCE HN001
- [SDR REXA2024011600079](https://openairdocs.org/sdr/REXA2024011600079.md): Intercostal · corroded · Nov 15, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT 26L BETWEEN FS 865.00 AND 881.00 IS CORRODED. REMOVED CORROSION AT INTERCOSTAL AT 26L BETWEEN FS 865.00 AND 881.00 IAW CRJ900 SRM 51-21-06-001-001-A01.
- [SDR REXA2024103101285](https://openairdocs.org/sdr/REXA2024103101285.md): Frame · corroded · Nov 14, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT F.S. 645 STGR 17L TO STGR 18L IS CORRODED ON THE FWD AND AFT SIDE. REMOVED CORRODED FRAME AT F.S.645 FROM STGR 17L TO STGR 18L AND INSTALLED NEW SERVICABLE FRAME P/N SH690-33126-1B IAW CRJ 900 SRM 53-00-06-201-001-A03.
- [SDR REXA2023112000983](https://openairdocs.org/sdr/REXA2023112000983.md): Nut Plate · corroded · Nov 13, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > 4 NUT-PLATES ARE CORRODED BETWEEN F.S. 661+16 TO F.S.661+32 BETWEEN STGR 26L AND 24R. INSTALLED 4 FASTENERS AND 1 RETAINER PLATE P/N SH670-39095-7 FROM F.S. 661+16 TO F.S. 661+32 BETWEEN STGR 26L TO STGR 24R IAW CRJ900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024110101387](https://openairdocs.org/sdr/REXA2024110101387.md): Cleat · corroded · Nov 9, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR CLEAT ON FWD DD4 AND FS 320 CORRODED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR CLEAT P/N:600-31902-269 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2024103101284](https://openairdocs.org/sdr/REXA2024103101284.md): Stub Frame · corroded · Nov 5, 2023 · N607LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 661 STUB FRAME UNDER CENTER CARGO DOOR SILL IS CORRODED BETWEEN STGR 25L AND 26L REMOVED AND REPLACED STUB FRAME P/N SH670-33824-1 IAW CRJ 900 SRM 51-42-21-001-001-A01
- [SDR REXA2024061400431](https://openairdocs.org/sdr/REXA2024061400431.md): Door Frame · corroded · Nov 5, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR AFT FORMER CORRODED WHERE POWER ASSIST MOTOR PULLEY BRACKET IS LOCATED RECEIVED AND COMPLIED WITH ENDEAVOR EA CRJ953-15781 REV A.
- [SDR REXA2024061400430](https://openairdocs.org/sdr/REXA2024061400430.md): Intercostal · corroded · Nov 5, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD INTERCOSTAL DD3 CORRODED REMOVED AND REPLACED WITH NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD3 P/N:601R318054-1 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2024061400429](https://openairdocs.org/sdr/REXA2024061400429.md): Intercostal · corroded · Nov 5, 2023 · N607LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD INTERCOSTAL DD1 CORRODED REMOVED AND REPLACED WITH NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD1 P/N:601R318054-1 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR REXA2023112000989](https://openairdocs.org/sdr/REXA2023112000989.md): Stringer Fitting · corroded · Nov 3, 2023 · N607LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R SPLICE AT F.S. 333 IS HEAVILY CORRODED. REMOVED CORRODED STRINGER SPLICE AND INSTALLED A NEW STRINGER SPLICE #23 (P/N: SH670-32429-4) IAW CRJ900 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01.
- [SDR REXA2024011600078](https://openairdocs.org/sdr/REXA2024011600078.md): Seat Track · corroded · Nov 2, 2023 · N607LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT RAIL IS CORRODED BETWEEN F.S. 364 TO F.S. 485 THE SEAT RAIL AT LBL 9 BETWEEN F.S. 364 TO F.S. 485.AT WAS REMOVED AND REPLACED IAW CRJ900 AMM 53-00-49-000/400-801 A07.

Next page: https://openairdocs.org/aircraft/N607LR/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N607LR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N607LR/reports

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